US3897588A - Process for the production of laminates utilizing pre-treating followed by impregnation - Google Patents

Process for the production of laminates utilizing pre-treating followed by impregnation Download PDF

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US3897588A
US3897588A US331030A US33103073A US3897588A US 3897588 A US3897588 A US 3897588A US 331030 A US331030 A US 331030A US 33103073 A US33103073 A US 33103073A US 3897588 A US3897588 A US 3897588A
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glass
sheets
production
weight
prepregs
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Touru Nohtomi
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Mitsubishi Gas Chemical Co Inc
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Mitsubishi Gas Chemical Co Inc
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    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21HPULP COMPOSITIONS; PREPARATION THEREOF NOT COVERED BY SUBCLASSES D21C OR D21D; IMPREGNATING OR COATING OF PAPER; TREATMENT OF FINISHED PAPER NOT COVERED BY CLASS B31 OR SUBCLASS D21G; PAPER NOT OTHERWISE PROVIDED FOR
    • D21H19/00Coated paper; Coating material
    • D21H19/02Metal coatings
    • D21H19/04Metal coatings applied as foil
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/08Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different fibres
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21HPULP COMPOSITIONS; PREPARATION THEREOF NOT COVERED BY SUBCLASSES D21C OR D21D; IMPREGNATING OR COATING OF PAPER; TREATMENT OF FINISHED PAPER NOT COVERED BY CLASS B31 OR SUBCLASS D21G; PAPER NOT OTHERWISE PROVIDED FOR
    • D21H27/00Special paper not otherwise provided for, e.g. made by multi-step processes
    • D21H27/30Multi-ply
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00Printed circuits
    • H05K1/02Details
    • H05K1/03Use of materials for the substrate
    • H05K1/0313Organic insulating material
    • H05K1/0353Organic insulating material consisting of two or more materials, e.g. two or more polymers, polymer + filler, + reinforcement
    • H05K1/036Multilayers with layers of different types
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00Printed circuits
    • H05K1/02Details
    • H05K1/03Use of materials for the substrate
    • H05K1/0313Organic insulating material
    • H05K1/0353Organic insulating material consisting of two or more materials, e.g. two or more polymers, polymer + filler, + reinforcement
    • H05K1/0366Organic insulating material consisting of two or more materials, e.g. two or more polymers, polymer + filler, + reinforcement reinforced, e.g. by fibres, fabrics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02Composition of the impregnated, bonded or embedded layer
    • B32B2260/021Fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04Impregnation, embedding, or binder material
    • B32B2260/046Synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/06Vegetal fibres
    • B32B2262/062Cellulose fibres, e.g. cotton
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/101Glass fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/306Resistant to heat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/732Dimensional properties
    • B32B2307/734Dimensional stability
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21HPULP COMPOSITIONS; PREPARATION THEREOF NOT COVERED BY SUBCLASSES D21C OR D21D; IMPREGNATING OR COATING OF PAPER; TREATMENT OF FINISHED PAPER NOT COVERED BY CLASS B31 OR SUBCLASS D21G; PAPER NOT OTHERWISE PROVIDED FOR
    • D21H11/00Pulp or paper, comprising cellulose or lignocellulose fibres of natural origin only
    • D21H11/02Chemical or chemomechanical or chemothermomechanical pulp
    • D21H11/04Kraft or sulfate pulp
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21HPULP COMPOSITIONS; PREPARATION THEREOF NOT COVERED BY SUBCLASSES D21C OR D21D; IMPREGNATING OR COATING OF PAPER; TREATMENT OF FINISHED PAPER NOT COVERED BY CLASS B31 OR SUBCLASS D21G; PAPER NOT OTHERWISE PROVIDED FOR
    • D21H11/00Pulp or paper, comprising cellulose or lignocellulose fibres of natural origin only
    • D21H11/12Pulp from non-woody plants or crops, e.g. cotton, flax, straw, bagasse
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21HPULP COMPOSITIONS; PREPARATION THEREOF NOT COVERED BY SUBCLASSES D21C OR D21D; IMPREGNATING OR COATING OF PAPER; TREATMENT OF FINISHED PAPER NOT COVERED BY CLASS B31 OR SUBCLASS D21G; PAPER NOT OTHERWISE PROVIDED FOR
    • D21H13/00Pulp or paper, comprising synthetic cellulose or non-cellulose fibres or web-forming material
    • D21H13/36Inorganic fibres or flakes
    • D21H13/38Inorganic fibres or flakes siliceous
    • D21H13/40Inorganic fibres or flakes siliceous vitreous, e.g. mineral wool, glass fibres
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21HPULP COMPOSITIONS; PREPARATION THEREOF NOT COVERED BY SUBCLASSES D21C OR D21D; IMPREGNATING OR COATING OF PAPER; TREATMENT OF FINISHED PAPER NOT COVERED BY CLASS B31 OR SUBCLASS D21G; PAPER NOT OTHERWISE PROVIDED FOR
    • D21H17/00Non-fibrous material added to the pulp, characterised by its constitution; Paper-impregnating material characterised by its constitution
    • D21H17/20Macromolecular organic compounds
    • D21H17/33Synthetic macromolecular compounds
    • D21H17/46Synthetic macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21HPULP COMPOSITIONS; PREPARATION THEREOF NOT COVERED BY SUBCLASSES D21C OR D21D; IMPREGNATING OR COATING OF PAPER; TREATMENT OF FINISHED PAPER NOT COVERED BY CLASS B31 OR SUBCLASS D21G; PAPER NOT OTHERWISE PROVIDED FOR
    • D21H17/00Non-fibrous material added to the pulp, characterised by its constitution; Paper-impregnating material characterised by its constitution
    • D21H17/20Macromolecular organic compounds
    • D21H17/33Synthetic macromolecular compounds
    • D21H17/46Synthetic macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
    • D21H17/47Condensation polymers of aldehydes or ketones
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K2201/00Indexing scheme relating to printed circuits covered by H05K1/00
    • H05K2201/01Dielectrics
    • H05K2201/0137Materials
    • H05K2201/0166Polymeric layer used for special processing, e.g. resist for etching insulating material or photoresist used as a mask during plasma etching
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K2201/00Indexing scheme relating to printed circuits covered by H05K1/00
    • H05K2201/02Fillers; Particles; Fibers; Reinforcement materials
    • H05K2201/0275Fibers and reinforcement materials
    • H05K2201/0284Paper, e.g. as reinforcement
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K2201/00Indexing scheme relating to printed circuits covered by H05K1/00
    • H05K2201/02Fillers; Particles; Fibers; Reinforcement materials
    • H05K2201/0275Fibers and reinforcement materials
    • H05K2201/0293Non-woven fibrous reinforcement
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K2201/00Indexing scheme relating to printed circuits covered by H05K1/00
    • H05K2201/03Conductive materials
    • H05K2201/0332Structure of the conductor
    • H05K2201/0335Layered conductors or foils
    • H05K2201/0355Metal foils
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K2203/00Indexing scheme relating to apparatus or processes for manufacturing printed circuits covered by H05K3/00
    • H05K2203/14Related to the order of processing steps
    • H05K2203/1476Same or similar kind of process performed in phases, e.g. coarse patterning followed by fine patterning
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/901Printed circuit
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31511Of epoxy ether
    • Y10T428/31529Next to metal
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31551Of polyamidoester [polyurethane, polyisocyanate, polycarbamate, etc.]
    • Y10T428/31627Next to aldehyde or ketone condensation product

Definitions

  • This invention relates to aprocess for the production of laminates. More particularly, it relates to a process for the manufacture of a laminate having superior machinability, heat resistance and dimensional stability characterized by pre-treating sheets made of mixed glass and cellulose fibers, with a melamine resin and/or a phenolic resin having relatively many methylol groups in the molecule, thereafter impregnating the pre-treated sheets with a thermosetting resin and then laminating the impregnated sheets alone or together with glass fabric previously treated with a thermosetting resin.
  • Glass fabric-base epoxy laminates have heretofore been used as a base material for printed circuits or insulators for use in highly delicate electronic apparatuses such as electronic computers and controllers.
  • laminates having an improved machinability there have been proposed glass fiber-base epoxy laminates consisting essentially of non-woven and woven glass fabrics (see Japanese Utility Model Gazette 32228/68). These laminates are somewhat improved but still unsatisfactory in machinability and are poor in dimensional stability due to their increased content of non-woven glass fabrics.
  • non-woven cloths are webs or mats in which the fibers arranged in parallel, crosswise or at random with respect to each other are together bonded by the use of a suitable binder.
  • the suitable binder is usually a watersoluble binder, and non-woven glass fabrics are thus in ferior in waterproof property and heat resistance.
  • Japanese Patent Gazette 9957/71 there is disclosed a process for the manufacture ofa laminate which is made of non-woven glass fabrics and glass fabrics and in which the positioning and amount of the non-woven glass fabrics used are specified, the process being intended to thereby produce new laminates which are the same as those described in said Japanese Utility Model Gazette 32228/68 except that the new laminates are improved in dimensional stability.
  • Laminates produced by this process are improved in dimensional stability and, on the other hand, they are deteriorated in machinability due to their increased content of glass fabrics and are not sufficiently improved in waterproof property and heat resistance due to the use of non-woven glass fabrics as the base material.
  • the object of this invention can be accomplished by using as the base material a plurality of glass-cellulose sheets made of 20-70% by weight of cellulose fibers and 30-80% by weight of glass fibers and employing the following three steps:
  • the object of this invention will neither be attained unless a base material is subjected to such pretreatment as the step (1) even if the base material is glass-cellulose sheets according to this invention, nor will it be attained if the base material is other than the specified one according to this invention even if the base material is preliminarily treated with a melamine resin and/or a methylol group-rich phenolic resin.
  • the glass-cellulose sheets as the base material as well as the use of the above-mentioned three steps to obtain a laminate having excellent machinability, heat resistance, dimensional stability and electrical properties.
  • the glass-cellulose sheets which may be used as the base material in the practice of this invention are those obtained by making cellulosic and glass fibers into paper-like sheets. They contain none of such binders as used in conventional non-woven glass fabrics and consist solely of cellulosic and glass fibers. Thus, they are a substance distinct from the non-woven glass fabrics and are different in properties therefrom; for instance, the former have larger tensile strength than the latter.
  • Glass fibers for general use in the glass-cellulose sheets are about 5 to l3,u in diameter and 5 to 30 mm in length.
  • Cellulose fibers which may be used include linters, kraft fibers and the mixtures thereof with the linters being preferable.
  • the glass-cellulose fiber sheets according to this invention should contain glass fibers in amounts of 3080%, preferably 40-80% and more preferably 60-70% by weight.
  • the use of glass fibers in amounts of less than 30% by weight will give a laminate having decreased electrical properties and heat resistance and, on the other hand, the use of more than by weight of glass fibers will produce a laminate having decreased machinability and dimensional stability.
  • the pre-treatment of the glass-cellullose sheets is to impregnate them with a varnish of a melamine resin and/or a methylol group-rich phenolic resin and then dry the impregnated sheets.
  • the melamine resins which may be used in this pretreatment step are those which are prepared from formaldehyde and melamine in a molar ratio of from 1 to 6, preferably, from 1 to at least 3 in the presence of acid catalyst.
  • Methyl group-rich phenolic resins which may be used are those which are prepared from formaldehyde and phenol in a molar ratio of from 1.3 to 3.0, preferably from 1.5 to 3.0 and more preferably from 2.0 to 2.5 in the presence of a1 kali catalyst.
  • phenolic resins prepared from formaldehyde and phenol in a molar ratio of from 1 to 1.3 willgive laminates having lowered electrical properties.
  • the methylol group-rich phenolic resins have 1.7 to 2.7 methylol groups in the nucleus.
  • the resins employed in the pre-treating step the methylol Amount by weight of resin impregnated Weight of base material Amount by weight of resin impregnated is in the range of from 2 to 40%, preferably from 5 to l by weight of the pre-treated sheets.
  • the glass-cellulose sheets may, prior to the pre-treating step, be treated with Volane (methacrylatechromic chloride) or silane, with the silane being preferred.
  • Volane methacrylatechromic chloride
  • silane silane
  • the pre-treated sheets are impregnated with a varnish of a thermosetting resin and dried to obtain a prepreg.
  • Thermosetting resins which may be used in the impregnating step include the usual ones such as epoxy,
  • Total amount by weight of resins impregnated is in the range of 3080% by weight, preferably 70% by weight of the prepregs.
  • the use of the total resins in amounts of less than 30% by weight will produce the laminates having lowered electric properties and, on the other hand, the total resin in amount of ity, heat resistance, dimensional stability and electrical 5 properties.
  • the inner layer or layers of the laminate may contain other glass fabric.
  • said inner layer or layers should preferably 6 consist solely of the glass-cellulose sheets to allow the laminate to have excellent maehinability.
  • the abovementioned pretreating condition according to this invention may be effected at temperatures of to C, for 5 to 15 minutes, and the impregnating condition may be effected at temperatures of 100 to C, for 5 to 15 minutes.
  • the resins which may be used in treating the glass fabrics may be the thermosetting resins as used in the impregnation of glass-cellulose sheets.
  • the thermosetting resins include epoxy, phemolic. polyimide, poly- 5 amide and polyester resins. Among these resins, an
  • epoxy resin is especially preferred.
  • the amount of resin impregnated into the glass fabric represented by the formula Am tb wei ht of resn im re nat d oun y g I p g e x 100% is in the range of 20-80% by weight, preferably 30-60% by weight of glass fabric prepreg.
  • the use of less than 20% by Weight of the resin will produce the laminate of lowered electrical properties, while the use of more than 80% by weight thereof will result in lowered moldability.
  • the laminates of glass-cellulosic sheets or those wherein the outermost surfaces are covered with the glass fabric If desired, there can also be obtained such laminates wherein at least one of the outermost surfaces is further covered with a metallic foil such as copper or nickel foil.
  • the lamination according to this invention may be effected at a temperature of l40l 80C and pressure of 20-150 kg/cm for a time length of 30-120 minutes.
  • FIGS. 1 to 4 generally show the insulation resistance, heat resistance, shearing stress and dimensional stability of various laminates produced using as the base material various glass-cellulose sheets wherein the mixing ratio of the glass and cellulose fibers is varied and under the same conditions as in the following Examples. These FIGURES will be detailed as follows.
  • FIG. 1 shows the variations of the insulation resistance with varying proportion of glass fibers in glasscellulose sheets, as measured by the method prescribed (Japanese Industrial Standard-C- 6481), the variation (A) being for the laminate as received and the other (B) for the same one after boiled for two hours. It is seen that when the proportion of glass fibers is small the insulation resistance after 2 hours boiling is considerably lowered;
  • FIG. 2 shows the variations of solder resistance at 260C with varying proportion of glass fibers in glasscellulose sheets, the variation (A) being for the laminate as received and the other (B) for the same one after boiled for 2 hours, and shows that when the proportion of glass fibers is less than 30% the solder resistance remarkably decreases;
  • FIG. 3 shows the variation of shearing stress at room temperature, which is an indicator of machinability, with varying proportion of glass fibers in glass-cellulose sheets, and also indicates that when'the proportion of glass fibers is more than 80% the shearing stress sharply increases thereby requiring a powerful stamping press for punching the laminate, increasing the wear of a mold used and causing thecracking and peeling of the laminate; and
  • FIG. 4 shows the variation of scatter of the thickness of laminates obtained by laminating,'with varying proportion of glass fibers in glass-cellulose sheets, the scatter of the thickness being represented by the formula Maximum thicknessMinimum thickness
  • the FIGURE indicates that the use of more than 90% by weight of glass fibers in the laminates sharply increases the scatter of the thickness thereof.
  • Table 1 shows the comparison of-properties between the laminates (Example 1) produced according to this invention, those (Comparison example 1) produced from the glass-cellulose sheets without the pretreatment as previously mentioned and the conventional ones (Comparison example 2) produced from non-woven glass fabrics.
  • the laminates produced from the glass-cellulose sheets without the pretreatment are inferior in various properties to the conventional ones produced from the non-woven glass fabrics, while those produced from the glass-cellulose sheets after being subjected to the pre-treatment according to this invention are superior to said conventional ones in machinability, heat resistance and dimensional stability and electrical properties.
  • such superior laminates can be produced at a lower cost.
  • EXAMPLE 1 Glass cellulose sheets (0.25 mm thick) composed of 40% of cellulose fibers and of glass fibers were impregnated with aphenolic resin prepared from formaldehyde and phenol in the molar ratio of 2.5 and the resulting impregnated sheets were dried. The sheets thus pre-treated were impregnated with a heat resistant epoxy resin and then dried to form glass-cellulose sheet (or paper) prepregs (0.3 mm thick).
  • Glass fabrics (0.18 mm thick) were impregnated with a heat resistant epoxy resin and then dried to form glass fabric prepregs.
  • Eight of said glass-cellulose sheet prepregs were piled one upon another, the uppermost and lowermost layers of the resulting pile were each coverd with the glass fabric prepreg and then said fabric prepregs were each further covered with a copper foil to form a mass for lamination which was then laminated at a temperature of 160C and pressure of 40 kg/cm for a time length of 90 minutes thereby obtaining a copper-clad laminate.
  • the laminates thus obtained were tested and the results were shown in Table 1.
  • Glass-cellulose sheets (0.25 mm thick) composed of 40% of cellulose fibers and 60% of glass fibers were impregnated with a heat resistant epoxy resin without the pre-treatment according to this invention and were then dried to form glass-cellulose paper (or sheet) prepregs (0.3 mm thick), and glass fabric prepregs were prepared in the same manner as in Example 1.
  • the sheet prepregs and the glass. fabric prepregs were treated as in Example 1 to form a copper-clad laminate having the same thickness as the one in Example 1.
  • the properties of the thus-formed laminate are indicated in Table l.
  • Non-woven glass fabrics (0.25 mm thick) were impregnated with a heat resistant epoxy resin without the pre-treatment according to this invention and then dried to form non-woven glass fabric prepregs (0.3 mm thick), while glass fabrics were treated under the same conditions as in Example 1 to form glass fabric pre pregs.
  • Non-woven glass fabric prepregs and the glass fabric prepregs were treated as in Example 1 to obtain a copper-clad laminate having the same thickness as the one obtained in Example 1.
  • the properties of the laminate of Comparison example 2 are also shown in Table 1.
  • EXAMPLE 2 Glass-cel1ulose sheets (0.25 mm thick) composed of 30% by weight of cellulose fibers and 70% by weight of glass fibers were pre-treated with a phenolic resin as in Example 1, impregnated with an epoxy resin as in Example 1 and then dried to form glass-cellulose prepregs.
  • the laminate had'an insulation resistance of 3.8 X 10 in the as-received state and 4.9 X 10 after boiled for 2 hours; a surface resistance of 8.6 X 10 in the as-received state and 6.2 X 9 after exposed to C under a 90% RH, for 96 hours; a volume resistivity of 9.2 X 10().cm in as-received state and 5.7 X 10Q.cm after exposed to 40C under a 90% RH. for 96 hours; and a solder resistance of at least 120 sec. at 260C and 80-100 see. after boiled for 2 hours.
  • Example 3 Glass-cellulose sheets as in Example 1 were pretreated with a melamine resin prepared from formaldehyde and a modified melamine (Melolam 297). The pre-treated sheets were impregnated with an epoxy resin as in Example 1 and then dried to form glasscellulose sheet prepregs. Said prepregs were treated in the same manner as in Example 1 to obtain a copperclad laminate.
  • a melamine resin prepared from formaldehyde and a modified melamine (Melolam 297).
  • the pre-treated sheets were impregnated with an epoxy resin as in Example 1 and then dried to form glasscellulose sheet prepregs. Said prepregs were treated in the same manner as in Example 1 to obtain a copperclad laminate.
  • the laminate had an insulation resistance of 2.5 X 10"! in the as-received state and 1.5 X l0 fl after boiled for 2 hours; a surface resistance of 6.4 X 10! in the as-received state and 4.0 X 10 after exposed to 40C under a 90% RH, for 96 hours; a volume resistivity of 5.8 X 10Q.cm in the as-received state and 5.0 X l0' Q.cm after exposed to 40C under a 90% RH, for 96 hours; and a solder resistance of at least 120 sec. at 260C and -100 see. after boiled for 2 hours.
  • Example 4 Glass-cellulose sheets as in Example 1 were pretreated with a phenolic resin prepared from formaldehyde and phenol in the molar ratio of 2. The sheets so pre-treated were then treated in the same manner as in Example 1 to obtain acopper-clad laminate.
  • the laminate showed an insulation resistance of 3.1 X 10 0 in the as-received state and 7.8 X 10 9 after boiled for 2 hours; a surface resistance of 1.3 X [0' 0 in the as-received state and 2.7 X 10!) after exposed to 40C under a RH, for 96 hours; a volume resistivity of 2.5 X 10Q.cm in the as-received state and 4.8 X l0 Q.cm after exposed to 40C under a 90% RH. for 96 hours; and a solder resistance of at least sec. at 260C and 80-100 see. after boiled for 2 hours.
  • Example 5 The procedure of Example 1 was followed, except that the copper foil was substituted by a nickel foil (0.035 mm thick) to obtain a nickel-clad laminate.
  • the laminate showed an insulation resistance of 2.6 X 10 0 in the as-received state and 1.4 X 10 after boiled for 2 hours; a surface resistance of 4.9 X 10 Q in the as-received state and 2.7 X 10 0 after exposed to 40C under a 90% RH, for 96 hours; a volume resistivity of 7.1 X 10Q.cm in the as-received state and 3.5 X 10Q.cm after exposed to 40C under a 90% RH, for 96 hours; and a solder resistance of at least 120 sec. at 260C and 90-120 sec. after boiled for two hours.
  • a process for the production of metal-clad laminates comprising the steps of:
  • thermosetting synthetic resin impregnating the pre-treated sheets with a thermosetting synthetic resin
  • thermosetting used in the impregnating step is an epoxy resin
  • metal foil is selected from the group consisting of copper and nickel.
  • glass-cellulose sheets are composed of 20 to 60% by weight of cellulose fibers and 40 to 80% by weight of glass fibers.
  • a metal-clad laminate obtained by the process of claim 2.
  • a process according to claim 1 including the step of drying said glass cellulose sheets after said pretreating step and before said impregnating step.
  • a process according to claim 2 including the step of drying said glass cellulose sheets after said pretreating step and before said impregnating step.

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  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
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  • Inorganic Insulating Materials (AREA)

Abstract

A process for the production of laminates composed of sheets made of cellulose and glass fibers by pre-treating the sheets with a melamine resin or a methylol group-rich phenolic resin, impregnating the pre-treated sheets with a thermosetting resin and then laminating the impregnated sheets to produce the laminates. In one embodiment, the laminates are covered with a resin-treated glass fabric on at least one of the outermost surfaces or are further covered with a copper foil on the glass fabric-covered surface.

Description

United States Patent [1 1- Nohtomi 1 PROCESS FOR THE PRODUCTION OF LAMINATES UTILIZING PRE-TREATING FOLLOWED BY IMPREGNATION [7 51 Inventor:
[73] Assignee: Mitsubishi Gas Chemical Co., Inc.,
Tokyo, Japan 22 Filed: Feb. 9, 1973 211 App1.No.:331,030
Touru Nohtomi, Tokyo, Japan [30] Foreign Application Priority Data Feb. 12, 1972 Japan 47-14333 [52] US. Cl. 428/436; 156/309; 156/330; 156/335; 162/145; 428/418; 428/901 [51] Int.Cl. ..'.B32B17/10;B32B27/121B32B27/38; B32B 27/42 [58] Field of Search 156/309, 335, 330; 161/93, 161/155,170,193,196,198, DIG. 4, 186,
DIG. 7; 162/145 [56] References Cited UNITED STATES PATENTS 2,859,109 1 1/1958 I-Iawley et al. 162/145 1 July 29, 1975 3,228,825 l/1966 Waggoner 162/145 3,393,117 7/1968 Zolg et a1 161/82 3,560,328 2/1971 Anderson et a1. 161/251 3,617,613 11/1971 Benzinger et a1. 174/685 Primary ExaminerDoug1as J. Drummond Assistant Examiner-Robert A. Dawson Attorney, Agent, or Firm-Frank J. Jordan [57] ABSTRACT 19 Claims, 4 Drawing Figures PATENTED JUL 2 9 i975 's'o' '100 Proportion of glass fibers 2.3 wocm mmmwh cozm m 100 Proportion of glass fibers m E .6 mmwcxg 6 bwzmom Fig.1
' 's'o' '100 Proportion of glassfibers Proportion of glass fibers A EuBmmw m mcrmwcm 0/.) Fig .3
Fig.4
PROCESS FOR THE PRODUCTION OF LAMINATES UTILIZING PRE-TREATING FOLLOWED BY IMPREGNATION This invention relates to aprocess for the production of laminates. More particularly, it relates to a process for the manufacture of a laminate having superior machinability, heat resistance and dimensional stability characterized by pre-treating sheets made of mixed glass and cellulose fibers, with a melamine resin and/or a phenolic resin having relatively many methylol groups in the molecule, thereafter impregnating the pre-treated sheets with a thermosetting resin and then laminating the impregnated sheets alone or together with glass fabric previously treated with a thermosetting resin.
Glass fabric-base epoxy laminates have heretofore been used as a base material for printed circuits or insulators for use in highly delicate electronic apparatuses such as electronic computers and controllers. However, it is disadvantageous that they are unsatisfactory in machinability and are especially difficult to subject to cold punching. Thus, as laminates having an improved machinability, there have been proposed glass fiber-base epoxy laminates consisting essentially of non-woven and woven glass fabrics (see Japanese Utility Model Gazette 32228/68). These laminates are somewhat improved but still unsatisfactory in machinability and are poor in dimensional stability due to their increased content of non-woven glass fabrics. Such non-woven cloths are webs or mats in which the fibers arranged in parallel, crosswise or at random with respect to each other are together bonded by the use of a suitable binder. The suitable binder is usually a watersoluble binder, and non-woven glass fabrics are thus in ferior in waterproof property and heat resistance.
Further, in Japanese Patent Gazette 9957/71, there is disclosed a process for the manufacture ofa laminate which is made of non-woven glass fabrics and glass fabrics and in which the positioning and amount of the non-woven glass fabrics used are specified, the process being intended to thereby produce new laminates which are the same as those described in said Japanese Utility Model Gazette 32228/68 except that the new laminates are improved in dimensional stability. Laminates produced by this process are improved in dimensional stability and, on the other hand, they are deteriorated in machinability due to their increased content of glass fabrics and are not sufficiently improved in waterproof property and heat resistance due to the use of non-woven glass fabrics as the base material.
As a result of various studies made by the present inventors in an attempt to eliminate the disadvantages of the conventional laminates, it has been found that both the use of sheets made of mixed glass and cellulose fibers (the sheets being hereinafter referred to as glasscellulose sheets) as the base material, and the pretreatment of the glass-cellulose sheets with a melamine resin and/or a phenolic resin having relatively many methylol groups in the molecule (the phenolic resin being hereinafter referred to as methylol group-rich phenolic resin) prior to the impregnation of the sheets with a thermosetting resin will lead to the production of a laminate of the glass-cellulose sheets, which laminate has superior machinability, heat resistance and dimensional stability without damaging 'its electrical properties.
More particularly, the object of this invention can be accomplished by using as the base material a plurality of glass-cellulose sheets made of 20-70% by weight of cellulose fibers and 30-80% by weight of glass fibers and employing the following three steps:
1. pre-treating the glass-cellulose sheets with a melamine resin and/or a methylol group-rich phenolic resin,
2. impregnating the pre-treated sheets with a thermosetting resin and drying the impregnated sheets to form prepregs, and then 3. laminating the prepregs and glass fabrics so that the outermost surfaces of a laminate to be obtained are each covered with the glass fabric.
Thus, the object of this invention will neither be attained unless a base material is subjected to such pretreatment as the step (1) even if the base material is glass-cellulose sheets according to this invention, nor will it be attained if the base material is other than the specified one according to this invention even if the base material is preliminarily treated with a melamine resin and/or a methylol group-rich phenolic resin.
According to this invention, it needs the use of the glass-cellulose sheets as the base material as well as the use of the above-mentioned three steps to obtain a laminate having excellent machinability, heat resistance, dimensional stability and electrical properties.
The glass-cellulose sheets which may be used as the base material in the practice of this invention are those obtained by making cellulosic and glass fibers into paper-like sheets. They contain none of such binders as used in conventional non-woven glass fabrics and consist solely of cellulosic and glass fibers. Thus, they are a substance distinct from the non-woven glass fabrics and are different in properties therefrom; for instance, the former have larger tensile strength than the latter. Glass fibers for general use in the glass-cellulose sheets are about 5 to l3,u in diameter and 5 to 30 mm in length. Cellulose fibers which may be used include linters, kraft fibers and the mixtures thereof with the linters being preferable.
The glass-cellulose fiber sheets according to this invention should contain glass fibers in amounts of 3080%, preferably 40-80% and more preferably 60-70% by weight. The use of glass fibers in amounts of less than 30% by weight will give a laminate having decreased electrical properties and heat resistance and, on the other hand, the use of more than by weight of glass fibers will produce a laminate having decreased machinability and dimensional stability.
The pre-treatment of the glass-cellullose sheets is to impregnate them with a varnish of a melamine resin and/or a methylol group-rich phenolic resin and then dry the impregnated sheets. The melamine resins which may be used in this pretreatment step are those which are prepared from formaldehyde and melamine in a molar ratio of from 1 to 6, preferably, from 1 to at least 3 in the presence of acid catalyst. Methyl group-rich phenolic resins which may be used are those which are prepared from formaldehyde and phenol in a molar ratio of from 1.3 to 3.0, preferably from 1.5 to 3.0 and more preferably from 2.0 to 2.5 in the presence of a1 kali catalyst. The use of usual phenolic resins prepared from formaldehyde and phenol in a molar ratio of from 1 to 1.3 willgive laminates having lowered electrical properties. The methylol group-rich phenolic resins have 1.7 to 2.7 methylol groups in the nucleus. As the resins employed in the pre-treating step the methylol Amount by weight of resin impregnated Weight of base material Amount by weight of resin impregnated is in the range of from 2 to 40%, preferably from 5 to l by weight of the pre-treated sheets. The use ofless than 2% by weight of the resin in the pretreatment step Weight of glass fabric Amount by weight of resin impregnated will give the laminates having poor moisture resistance, while the use of more than 40% by weight thereof will give the laminates with lowered electrical properties 20 and heat resistance.
In addition, the glass-cellulose sheets may, prior to the pre-treating step, be treated with Volane (methacrylatechromic chloride) or silane, with the silane being preferred.
The pre-treated sheets are impregnated with a varnish of a thermosetting resin and dried to obtain a prepreg.
Thermosetting resins which may be used in the impregnating step, include the usual ones such as epoxy,
phenolic, polyimide, polyamide and polyester resins, with expoxy and phenolic resins being preferable and the former being more preferable.
The total amount of resins impregnated into the prepregs in the pre-treating and impregnating steps, represented by the formula Total amount by weight of resins impregnated Weight of base material Total amount by weight of resins impregnated is in the range of 3080% by weight, preferably 70% by weight of the prepregs. The use of the total resins in amounts of less than 30% by weight will produce the laminates having lowered electric properties and, on the other hand, the total resin in amount of ity, heat resistance, dimensional stability and electrical 5 properties.
In such a laminate covered with a glass fabric on at least one of the outermost surfaces, the inner layer or layers of the laminate may contain other glass fabric.
However, said inner layer or layers should preferably 6 consist solely of the glass-cellulose sheets to allow the laminate to have excellent maehinability. The abovementioned pretreating condition according to this invention may be effected at temperatures of to C, for 5 to 15 minutes, and the impregnating condition may be effected at temperatures of 100 to C, for 5 to 15 minutes.
The resins which may be used in treating the glass fabrics may be the thermosetting resins as used in the impregnation of glass-cellulose sheets. The thermosetting resins, include epoxy, phemolic. polyimide, poly- 5 amide and polyester resins. Among these resins, an
) epoxy resin is especially preferred.
The amount of resin impregnated into the glass fabric, represented by the formula Am tb wei ht of resn im re nat d oun y g I p g e x 100% is in the range of 20-80% by weight, preferably 30-60% by weight of glass fabric prepreg. The use of less than 20% by Weight of the resin will produce the laminate of lowered electrical properties, while the use of more than 80% by weight thereof will result in lowered moldability.
According to this invention, there can be obtained the laminates of glass-cellulosic sheets or those wherein the outermost surfaces are covered with the glass fabric. If desired, there can also be obtained such laminates wherein at least one of the outermost surfaces is further covered with a metallic foil such as copper or nickel foil.
The lamination according to this invention may be effected at a temperature of l40l 80C and pressure of 20-150 kg/cm for a time length of 30-120 minutes.
The features and advantages of this invention will be apparent to those skilled in the art from the following description of preferred embodiments thereof, taken in conjunction with the drawings.
In the drawings:
, FIGS. 1 to 4 generally show the insulation resistance, heat resistance, shearing stress and dimensional stability of various laminates produced using as the base material various glass-cellulose sheets wherein the mixing ratio of the glass and cellulose fibers is varied and under the same conditions as in the following Examples. These FIGURES will be detailed as follows.
FIG. 1 shows the variations of the insulation resistance with varying proportion of glass fibers in glasscellulose sheets, as measured by the method prescribed (Japanese Industrial Standard-C- 6481), the variation (A) being for the laminate as received and the other (B) for the same one after boiled for two hours. It is seen that when the proportion of glass fibers is small the insulation resistance after 2 hours boiling is considerably lowered;
FIG. 2 shows the variations of solder resistance at 260C with varying proportion of glass fibers in glasscellulose sheets, the variation (A) being for the laminate as received and the other (B) for the same one after boiled for 2 hours, and shows that when the proportion of glass fibers is less than 30% the solder resistance remarkably decreases;
FIG. 3 showsthe variation of shearing stress at room temperature, which is an indicator of machinability, with varying proportion of glass fibers in glass-cellulose sheets, and also indicates that when'the proportion of glass fibers is more than 80% the shearing stress sharply increases thereby requiring a powerful stamping press for punching the laminate, increasing the wear of a mold used and causing thecracking and peeling of the laminate; and t FIG. 4 shows the variation of scatter of the thickness of laminates obtained by laminating,'with varying proportion of glass fibers in glass-cellulose sheets, the scatter of the thickness being represented by the formula Maximum thicknessMinimum thickness The FIGURE indicates that the use of more than 90% by weight of glass fibers in the laminates sharply increases the scatter of the thickness thereof.
Table 1 shows the comparison of-properties between the laminates (Example 1) produced according to this invention, those (Comparison example 1) produced from the glass-cellulose sheets without the pretreatment as previously mentioned and the conventional ones (Comparison example 2) produced from non-woven glass fabrics.
As is apparent from Table l, the laminates produced from the glass-cellulose sheets without the pretreatment are inferior in various properties to the conventional ones produced from the non-woven glass fabrics, while those produced from the glass-cellulose sheets after being subjected to the pre-treatment according to this invention are superior to said conventional ones in machinability, heat resistance and dimensional stability and electrical properties.
In addition, according to this invention, such superior laminates can be produced at a lower cost.
This invention will be better understood by the following examples wherein all percentages are by weight unless otherwise specified.
EXAMPLE 1 Glass cellulose sheets (0.25 mm thick) composed of 40% of cellulose fibers and of glass fibers were impregnated with aphenolic resin prepared from formaldehyde and phenol in the molar ratio of 2.5 and the resulting impregnated sheets were dried. The sheets thus pre-treated were impregnated with a heat resistant epoxy resin and then dried to form glass-cellulose sheet (or paper) prepregs (0.3 mm thick).
Glass fabrics (0.18 mm thick) were impregnated with a heat resistant epoxy resin and then dried to form glass fabric prepregs. Eight of said glass-cellulose sheet prepregs were piled one upon another, the uppermost and lowermost layers of the resulting pile were each coverd with the glass fabric prepreg and then said fabric prepregs were each further covered with a copper foil to form a mass for lamination which was then laminated at a temperature of 160C and pressure of 40 kg/cm for a time length of 90 minutes thereby obtaining a copper-clad laminate. The laminates thus obtained were tested and the results were shown in Table 1.
Table 1 Example 1 Comparison Comparison example 1 example 2 Glass- Glass Non-woven Inner layer cellulose cellulose glass sheet sheet fabrics Constitution Glass Glass Glass Outer layers fabric fabric fabric Pre-treatment according to Prethis invention treated None None Finished thickness (mm) 1.6 1.6 1.6 Test for perforation by use of super hard drill (Number of 10000 2000 perforations) or more or less Solder resistance 120 40-50 120 260C (sec) As received or more or more After two -100 0-5 40-50 hours boiling Scatter of thickness of laminate 8 35 Insulation As received 3.0 X 10 1 9 X l0 6.3 X l0 resistance (0) I After two hours boiling 1.2 X 10 70 X 10" 1.1 X 10 As received 6.0 X l0" 3 l X 10 2.4 X 10 Surface resistance After exposure ((2) to 40C and 3.8 X 10 1.6 X 10 3.5 X10" RH for 96 hours Volume As received 8.3 X l0 2.0 X 10" 6.5 X 10" resistivity (0 cm) After exposure to 40C and 90% RH 4.2 X l0 4.9 X l0 8.2 X 10" 1 for 96 hours Peel strength of copper foil (kg/cm) 1.8-2.0 1.7-2.1 l.7-l.8 Flexural elastic modulus (kg/mm 2600 1700 Number of perforations made trimly in the laminate without causing cracks and peeling therein.
Glass-cellulose sheets (0.25 mm thick) composed of 40% of cellulose fibers and 60% of glass fibers were impregnated with a heat resistant epoxy resin without the pre-treatment according to this invention and were then dried to form glass-cellulose paper (or sheet) prepregs (0.3 mm thick), and glass fabric prepregs were prepared in the same manner as in Example 1. The sheet prepregs and the glass. fabric prepregs were treated as in Example 1 to form a copper-clad laminate having the same thickness as the one in Example 1. The properties of the thus-formed laminate are indicated in Table l.
COMPARISON EXAMPLE 2 Non-woven glass fabrics (0.25 mm thick) were impregnated with a heat resistant epoxy resin without the pre-treatment according to this invention and then dried to form non-woven glass fabric prepregs (0.3 mm thick), while glass fabrics were treated under the same conditions as in Example 1 to form glass fabric pre pregs. Non-woven glass fabric prepregs and the glass fabric prepregs were treated as in Example 1 to obtain a copper-clad laminate having the same thickness as the one obtained in Example 1. The properties of the laminate of Comparison example 2 are also shown in Table 1.
EXAMPLE 2 Glass-cel1ulose sheets (0.25 mm thick) composed of 30% by weight of cellulose fibers and 70% by weight of glass fibers were pre-treated with a phenolic resin as in Example 1, impregnated with an epoxy resin as in Example 1 and then dried to form glass-cellulose prepregs.
Eight of said prepregs were treated in the same manner as in Example 1 to obtain a copper-clad laminate.
The laminate had'an insulation resistance of 3.8 X 10 in the as-received state and 4.9 X 10 after boiled for 2 hours; a surface resistance of 8.6 X 10 in the as-received state and 6.2 X 9 after exposed to C under a 90% RH, for 96 hours; a volume resistivity of 9.2 X 10().cm in as-received state and 5.7 X 10Q.cm after exposed to 40C under a 90% RH. for 96 hours; and a solder resistance of at least 120 sec. at 260C and 80-100 see. after boiled for 2 hours.
EXAMPLE 3 Glass-cellulose sheets as in Example 1 were pretreated with a melamine resin prepared from formaldehyde and a modified melamine (Melolam 297). The pre-treated sheets were impregnated with an epoxy resin as in Example 1 and then dried to form glasscellulose sheet prepregs. Said prepregs were treated in the same manner as in Example 1 to obtain a copperclad laminate.
The laminate had an insulation resistance of 2.5 X 10"!) in the as-received state and 1.5 X l0 fl after boiled for 2 hours; a surface resistance of 6.4 X 10!) in the as-received state and 4.0 X 10 after exposed to 40C under a 90% RH, for 96 hours; a volume resistivity of 5.8 X 10Q.cm in the as-received state and 5.0 X l0' Q.cm after exposed to 40C under a 90% RH, for 96 hours; and a solder resistance of at least 120 sec. at 260C and -100 see. after boiled for 2 hours.
' EXAMPLE 4 Glass-cellulose sheets as in Example 1 were pretreated with a phenolic resin prepared from formaldehyde and phenol in the molar ratio of 2. The sheets so pre-treated were then treated in the same manner as in Example 1 to obtain acopper-clad laminate.
The laminate showed an insulation resistance of 3.1 X 10 0 in the as-received state and 7.8 X 10 9 after boiled for 2 hours; a surface resistance of 1.3 X [0' 0 in the as-received state and 2.7 X 10!) after exposed to 40C under a RH, for 96 hours; a volume resistivity of 2.5 X 10Q.cm in the as-received state and 4.8 X l0 Q.cm after exposed to 40C under a 90% RH. for 96 hours; and a solder resistance of at least sec. at 260C and 80-100 see. after boiled for 2 hours.
- EXAMPLE 5 The procedure of Example 1 was followed, except that the copper foil was substituted by a nickel foil (0.035 mm thick) to obtain a nickel-clad laminate.
The laminate showed an insulation resistance of 2.6 X 10 0 in the as-received state and 1.4 X 10 after boiled for 2 hours; a surface resistance of 4.9 X 10 Q in the as-received state and 2.7 X 10 0 after exposed to 40C under a 90% RH, for 96 hours; a volume resistivity of 7.1 X 10Q.cm in the as-received state and 3.5 X 10Q.cm after exposed to 40C under a 90% RH, for 96 hours; and a solder resistance of at least 120 sec. at 260C and 90-120 sec. after boiled for two hours.
EXAMPLE 6 The procedure of Example 1 was followed, but substituting the epoxy resin by the same phenolic resin as previously mentioned to obtain a copper-clad laminate which had the following properties:
Insulation resistance (in the as-received state) 4.8 X 10"!) (after 2 hrs boiling) 3.6 X 10!) Surface resistance 1.7 X 10".Q 3.8 X 10"0 Volume resistivity 1.0 X 10".(lcm 4.5 X 10.Q.cm
What is claimed is: l. A process for the production of laminates comprising the steps of:
pre-treating glass-cellulose sheets composed of 20-70% by weight of cellulosic fibers and 30-80% by weight of glass fibers with at least one member selected from the group consisting of melamine resins prepared from formaldehyde and melamine in a molar ratio of from 1 to 6 in the presence of an acid catalyst, and methylol group-rich phenolic resins prepared from formaldehyde and phenol in a molar ratio of from 1.3 to 3.0 in the presence of an alkali catalyst,
impregnating the pre-treated sheets with an epoxy resin,
drying the impregnated sheets to form prepregs thereof, arranging the prepregs for lamination, placing on the outermost ones of the arranged prepregs a glass fabric previously treated with the epoxy resin as used in the impregnation step, and
laminating the arranged prepregs with the resintreated glass fabric on the outermost prepregs to produce the laminate.
2. A process for the production of metal-clad laminates comprising the steps of:
pretreating glass-cellulose sheets composed of 70% by weight of cellulosic fibers and 30-80% by weight of glass fibers with at least one member selected from the group consisting of melamine resins prepared from formaldehyde and melamine in a molar ratio of from 1 to 6 in the presence of an acid catalyst, and methylol group-rich phenolic resins prepared from formaldehyde and phenol in a molar ratio of from 1.3 to 3.0 in the presence of an alkali catalyst,
impregnating the pre-treated sheets with a thermosetting synthetic resin,
drying the impregnated sheets to form prepregs thereof,
arranging the prepregs for lamination,
placing on the outer surface of each of the outermost ones of the arranged prepregs a glass fabric previously treated with the same thermosetting synthetic resin as used in the impregnating step,
covering with a metal foil the outer surface of at least one of the glass fabrics placed on said outermost prepregs, and
laminating the prepregs, glass fabrics and metal foil or foils so position to produce the metal-clad laminate.
3. A process for the production of laminates according to claim 1, wherein the amount of resin impregnated into the sheets in the pre-treating step is from 20 to 70% by weight of the sheets.
4. A process for the production of laminates according to claim 1, wherein the total amount of resins impregnated into the sheets in the pre-treating and impregnating steps is from 30 to 80% by weight ofthe prepregs.
5. A process for the production of metal-clad laminates according to claim 2, wherein the amount of resin impregnated into the sheets in the pre-treating step is from 20 to 70% by weight of the sheets.
6. A process for the production of metal-clad laminates according to claim 2, wherein the total amount of resins impregnated into the sheets in the pre-treating 10 and impregnating steps is from 30 to by weight of the prepregs.
7. A process for the production of laminates according to claim 1, wherein the amount of resin impregnated into the glass fabric is from 20 to 80% by weight thereof.
8. A process for the production of metal-clad lami nates according to claim 2, wherein the amount of resin impregnated into the glass fabric is from 20 to 80% by weight thereof.
9. A process for the production of laminates according to claim 1, wherein the methylol group-rich phenolic resins have 1.7 to 2.7 methylol groups in the nucleus.
10. A process for the production of metal-clad laminates according to claim 2, wherein the methylol group-rich phenolic resins have 1.7 to 2.7 methylol groups in the nucleus.
11. A process for the production of metal-clad 1aminates according to claim 2, wherein the thermosetting used in the impregnating step is an epoxy resin.
12. A process for the production of metal-clad laminates according to claim 2, wherein the metal foil is selected from the group consisting of copper and nickel.
13. A process for the production oflaminates according to claim 1, wherein the glass-cellulose sheets are composed of 20 to 60% by weight of cellulose fibers and 40 to 80% by weight of glass fibers.
14. A process for the production of metal-clad laminates according to claim 2, wherein the glass-cellulose sheets are composed of 20 to 60% by weight of cellulose fibers and 40 to 80% by weight of glass fibers.
15. A process for the production oflaminates according to claim 1, wherein the methylol group-rich phenolic resins are prepared from formaldehyde and phenol in a molar ratio of 1.5 to 3.0 in the presence of a1- kali catalyst.
16. A process for the production of metal-clad laminates according to claim 2, wherein the methylol group-rich phenolic resins are prepared from formaldehyde and phenol in a molar ratio of 1.5 to 3.0 in the presence of alkali catalyst.
17. A metal-clad laminate obtained by the process of claim 2.
18. A process according to claim 1 including the step of drying said glass cellulose sheets after said pretreating step and before said impregnating step.
19. A process according to claim 2 including the step of drying said glass cellulose sheets after said pretreating step and before said impregnating step.
l l l l

Claims (19)

1. A PROCESS FOR THE PRODUCTION OF LAMINATES COMPRISING THE STEPS OF: PRE-TREATING GLASS-CELLULOSE SHEETS COMPOSED OF 20-70% BY WEIGHT OF CELLULOSIC FIBERS AND 30-80% BY WEIGHT OF GLASS FIBERS WITH AT LEAST ONE MEMBER SELECTED FROM THE GROUP CONSISTING OF MELAMINE RESINS PREPARED FROM FORMALDEHYDE AND MELAMINE IN A MOLAR RATIO OF FROM 1 TO 6 IN THE PRESENCE OF AN ACID CATALYST, AND METHYLOL GROUP-RICH PHENOLIC RESINS PREPARED FROM FORMALDEHYDE AND PHENOL IN A MOLAR RATIO OF FROM 1.3 TO 3.0 IN THE PRESENCE OF AN ALKALI CATALYST, IMPREGNATING THE PRE-TREATED SHEETS WITH AN EPOXY RESIN, DRYING THE IMPREGNATED SHEETS TO FORM PREPREGS THEREOF, ARRANGING THE PREPREGS FOR LAMINATION, PLACING ON THE OUTERMOST ONES OF THE ARRANGED PREPREGS A GLASS FABRIC PREVIOUSLY TREATED WITH THE EPOXY RESIN AS USED IN THE IMPREGNATION STEP, AND LAMINATING THE ARRANGED PREPREGS WITH THE RESIN-TREATED GLASS FABRIC ON THE OUTERMOST PREPREGS TO PRODUCE THE LAMINATE.
2. A process for the production of metal-clad laminates comprising the steps of: pretreating glass-cellulose sheets composed of 20-70% by weight of cellulosic fibers and 30-80% by weight of glass fibers with at least one member selected from the group consisting of melamine resins prepared from formaldehyde and melamine in a molar ratio of from 1 to 6 in the presence of an acid catalyst, and methylol group-rich phenolic resins prepared from formaldehyde and phenol in a molar ratio of from 1.3 to 3.0 in the presence of an alkali catalyst, impregnating the pre-treated sheets with a thermosetting synthetic resin, drying the impregnated sheets to form prepregs thereof, arranging the prepregs for lamination, placing on the outer surface of each of the outermost ones of the arranged prepregs a glass fabric previously treated with the same thermosetting synthetic resin as used in the impregnating step, covering with a metal foil the outer surface of at least one of the glass fabrics placed on said outermost prepregs, and laminating the prepregs, glass fabrics and metal foil or foils so position to produce the metal-clad laminate.
3. A process for the production of laminates according to claim 1, wherein the amount of resin impregnated into the sheets in the pre-treating step is from 20 to 70% by weight of the sheets.
4. A process for the production of laminates aCcording to claim 1, wherein the total amount of resins impregnated into the sheets in the pre-treating and impregnating steps is from 30 to 80% by weight of the prepregs.
5. A process for the production of metal-clad laminates according to claim 2, wherein the amount of resin impregnated into the sheets in the pre-treating step is from 20 to 70% by weight of the sheets.
6. A process for the production of metal-clad laminates according to claim 2, wherein the total amount of resins impregnated into the sheets in the pre-treating and impregnating steps is from 30 to 80% by weight of the prepregs.
7. A process for the production of laminates according to claim 1, wherein the amount of resin impregnated into the glass fabric is from 20 to 80% by weight thereof.
8. A process for the production of metal-clad laminates according to claim 2, wherein the amount of resin impregnated into the glass fabric is from 20 to 80% by weight thereof.
9. A process for the production of laminates according to claim 1, wherein the methylol group-rich phenolic resins have 1.7 to 2.7 methylol groups in the nucleus.
10. A process for the production of metal-clad laminates according to claim 2, wherein the methylol group-rich phenolic resins have 1.7 to 2.7 methylol groups in the nucleus.
11. A process for the production of metal-clad laminates according to claim 2, wherein the thermosetting used in the impregnating step is an epoxy resin.
12. A process for the production of metal-clad laminates according to claim 2, wherein the metal foil is selected from the group consisting of copper and nickel.
13. A process for the production of laminates according to claim 1, wherein the glass-cellulose sheets are composed of 20 to 60% by weight of cellulose fibers and 40 to 80% by weight of glass fibers.
14. A process for the production of metal-clad laminates according to claim 2, wherein the glass-cellulose sheets are composed of 20 to 60% by weight of cellulose fibers and 40 to 80% by weight of glass fibers.
15. A process for the production of laminates according to claim 1, wherein the methylol group-rich phenolic resins are prepared from formaldehyde and phenol in a molar ratio of 1.5 to 3.0 in the presence of alkali catalyst.
16. A process for the production of metal-clad laminates according to claim 2, wherein the methylol group-rich phenolic resins are prepared from formaldehyde and phenol in a molar ratio of 1.5 to 3.0 in the presence of alkali catalyst.
17. A METAL-CLAD LAMINATE OBTAINED BY THE PROCESS OF CLAIM 2.
18. A process according to claim 1 including the step of drying said glass cellulose sheets after said pre-treating step and before said impregnating step.
19. A process according to claim 2 including the step of drying said glass cellulose sheets after said pre-treating step and before said impregnating step.
US331030A 1972-02-12 1973-02-09 Process for the production of laminates utilizing pre-treating followed by impregnation Expired - Lifetime US3897588A (en)

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US3987230A (en) * 1974-03-13 1976-10-19 Mitsubishi Gas Chemical Company, Inc. Laminates and process for production thereof
US4276328A (en) * 1978-11-04 1981-06-30 Ferodo Limited Impregnation of yarns
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US4360560A (en) * 1979-03-08 1982-11-23 Dynamit Nobel Aktiengesellschaft Base material for the production of printed circuits and process for the preparation of the base material
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US4654248A (en) * 1985-12-16 1987-03-31 Gte Communication Systems Corporation Printed wiring board with zones of controlled thermal coefficient of expansion
US4929494A (en) * 1986-03-05 1990-05-29 Showa Denko Kabushiki Kaisha Fibrous substrates impregnated with a curable composition
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US3987230A (en) * 1974-03-13 1976-10-19 Mitsubishi Gas Chemical Company, Inc. Laminates and process for production thereof
US4276328A (en) * 1978-11-04 1981-06-30 Ferodo Limited Impregnation of yarns
US4360560A (en) * 1979-03-08 1982-11-23 Dynamit Nobel Aktiengesellschaft Base material for the production of printed circuits and process for the preparation of the base material
US4370386A (en) * 1979-09-19 1983-01-25 Kanegafuchi Kagaku Kogyo Kabushiki Kaisha Reinforced unsaturated polyester resin laminate
EP0040848A1 (en) * 1980-05-26 1981-12-02 Kanegafuchi Kagaku Kogyo Kabushiki Kaisha Insulating laminate
US4370191A (en) * 1980-07-02 1983-01-25 Kanegafuchi Kagaku Kogyo Kabushiki Kaisha Electrical laminate
US4388129A (en) * 1980-09-22 1983-06-14 Kanegafuchi Kagaku Kogyo Kabushiki Kaisha Production of bubble-free electrical laminates
EP0050694A2 (en) * 1980-10-28 1982-05-05 Lcoa Laminating Company Of America Entry material and method for drilling circuit boards
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US4521491A (en) * 1980-12-02 1985-06-04 Kanegafuchi Kagaku Kogyo Kabushiki Kaisha Flame-retarded copper-clad laminate
US4513055A (en) * 1981-11-30 1985-04-23 Trw Inc. Controlled thermal expansion composite and printed circuit board embodying same
US4654248A (en) * 1985-12-16 1987-03-31 Gte Communication Systems Corporation Printed wiring board with zones of controlled thermal coefficient of expansion
US4929494A (en) * 1986-03-05 1990-05-29 Showa Denko Kabushiki Kaisha Fibrous substrates impregnated with a curable composition
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JPS4883170A (en) 1973-11-06

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